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HEAT EXCHANGE MODELING ON THE AIRCRAFT SURFACE UNDER HYPERSONIC SPEED OF THE APPROACH FLOW |
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| รหัสดีโอไอ | |
| Creator | A.A. Chernykh, A.I.Sharapov, A.V. Peshkova, Y.V. Shatskikh |
| Title | HEAT EXCHANGE MODELING ON THE AIRCRAFT SURFACE UNDER HYPERSONIC SPEED OF THE APPROACH FLOW |
| Contributor | - |
| Publisher | TuEngr Group |
| Publication Year | 2562 |
| Journal Title | International Transaction Journal of Engineering, Management, & Applied Sciences & Technologies |
| Journal Vol. | 10 |
| Journal No. | 5 |
| Page no. | 689-694 |
| Keyword | Heat flow on Aircraft, Aircraft simulation, Hypersonic flight speed, Hypersonic aircraft, Flow temperature, Heat exchange simulation, Navier-Stokes equations. |
| URL Website | http://tuengr.com/Vol10_5.html |
| Website title | ITJEMAST V10(5) 2019 @ TuEngr.com |
| ISSN | 2228-9860 |
| Abstract | The paper discusses the principles of modeling thermal interaction between aircraft protective coatings and approach flow. This work has developed software with relation to the flight of aircraft moving at high supersonic speeds combined functional setting for boundary conditions of various types particularly parameters of the atmosphere and hypersonic aircraft (HA) prototype material, reference flight conditions, parameters of the approach flow, etc. In this study, the hypersonic gas flow is considered as chemically nonequilibrium medium, which is an intermediate state of equilibrium and stagnated flows. The results from the numerical simulation of heat exchange on the winged vehicle surface at hypersonic flow rate are given. |
